Structural design of cyclocopter blade system

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 4, Issue , 2005, Pages 2743-2749

  Hwang, In Seong ^a,b   Hwang, Chang Sup ^a,b   Kim, Seung Jo ^a,b,c,d  

^a Seoul National University   (South Korea)

^b Seoul National University   (South Korea)

^c Flight Vehicle Research Center   (South Korea)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CYCLOCOPTER BLADE SYSTEMS; PLY ANGLES; ROTARY WING; STACKING SEQUENCE;

AERODYNAMICS; AIRFRAMES; OPTIMIZATION; ROTORS; STRESS ANALYSIS; STRUCTURAL DESIGN; WINGS;

TURBOMACHINE BLADES;

EID: 28844455032     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Yun, C.Y., "A New Vertical Take-off and Landing Aircraft with Cycloidal Blades System: Cyclocopter", Ph.D thesis, Seoul National University, 2004
2. th annual forum proceeding, Baltimore, MD, June 7-10, 2004
3. Wheatley, J.B. "Simplified Aerodynamic Analysis of the Cyclogiro Rotating-wing System", Technical Notes NACA No.467, August 1933
4. Kirsten, F.K. "Cycloidal propulsion in air", Bulletin No. 79, Engineering Experiment Station Series, University of Washington, March 1935
5. Gibbens, R.P. and Boschma, J.H. "Construction and testing of a new aircraft cycloidal propeller", 13th AIAA Lighter-Than-Air Systems Technology conference, Norfolk, VA June 28-July 1, AIAA No.99-3906,pp.1-9, 1999
6. Myers, R.H., Montgomery, D.C. Response surface methodology: process and product optimization using designed experiments, New York: Wiley, 1995
7. Gen, M., Cheng, R. Genetic algorithms and engineering optimization, New York: Wiley, 2000
8. nd Edition, Taylor & Francis, 1999
9. MSC.Patran 2003 PCL Reference Guide
10. Newman, S., The Foundations of Helicopter Flight, Edward Arnold, 1994